| 摘要 |
The present invention provides one pair or two pairs of horizontal propellers incorporated on the two opposite sides of an aircraft, which propellers by their rotating external blades create through their frontal shell opening a very strong frontal depression, stronger than their drag, providing an horizontal motion subsonic or supersonic, but their main advantage arise from the supersonic speed power requirement which is less than 20% of that of equivalent supersonic aircraft's, with consequent economy of construction, of maintenance and mainly in flight cost, and also a multiple in flight range and obviously respectively decrease of air pollution. Also if a vertical take-off and landing are required, these propellers by their internal blade could function as radial-flow propeller or blowers until their horizontal speed attains that required to support the aircraft by their wings, then by obstructing the radial-flow of the propeller and increasing the external blades rotation a supersonic speed is attained with the same economical and operational advantages of previous paragraph. And all that with only the present day technology.
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